Decoupling-type free vibration suspending structure of bridge segment model

A model and bridge technology, applied in the field of measurement equipment, can solve problems such as flutter derivative identification, and achieve the effect of convenient transportation and meeting stiffness requirements

Inactive Publication Date: 2011-09-07
HARBIN INST OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In order to solve the problem of flutter derivative identification of bridge segment models used in the prior art, the

Method used

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  • Decoupling-type free vibration suspending structure of bridge segment model
  • Decoupling-type free vibration suspending structure of bridge segment model
  • Decoupling-type free vibration suspending structure of bridge segment model

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Experimental program
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Embodiment Construction

[0027] Such as figure 1 As shown, the free vibration suspension structure of the decoupled bridge segment model is composed of a base 1, a main body support frame 2, a suspension device 3, and a tie rod 4.

[0028] Such as figure 2 As shown, the base 1 is composed of four square steels and rectangular blocks 5. The ends of the two short square steels are inserted into the rectangular blocks and fixed with nuts. The two ends of the rectangular steel are welded with connecting pieces. The connecting pieces can be bolted It is fixed on the rectangular block 5, and the bottom of the rectangular block has a hole to fix the whole base on the ground. The main body support frame 2 is composed of four vertical support shafts 6, four transverse connection shafts 7 and T-joints 8. The vertical support shaft adopts a segmented design, which is convenient for disassembly, installation and transportation. Each section of the support shaft is It is composed of a Φ10cm stainless steel solid ste...

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PUM

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Abstract

The invention relates to a decoupling-type free vibration suspending structure of a bridge segment model, which comprises a base, a body support rack, a pull rod, a bottom plate, a vertical guide post, a vertical sliding block, a spring connecting rod, a horizontal guide post, a horizontal sliding block, a rotating shaft, a force bearing disc and a connecting plate, wherein the spring connecting rod is respectively in threaded connection with upper and lower connecting shafts of the body support rack and two ends of the vertical sliding block; the bottom plate is fixed on two connecting shafts in the middle of the body support rack through threads, the vertical guide post is fixed on a support base of the bottom plate via a fastening screw, the vertical sliding block is inserted on the vertical guide post in a penetrating manner, the horizontal guide post is fixed at two ends of the vertical sliding block, the horizontal sliding block is inserted on the horizontal guide post in a penetrating manner, the force bearing disc is fixed on the rotating shaft via a flat key, and one end of the rotating shaft is inserted into the horizontal sliding block while the other end thereof is fixed with the connecting plate via a set screw. Three degrees of freedom in the structure of the invention can be locked independently, measurement can be carried out based on the desired degree of freedom, and with the spring tensioning forces in various directions being adjustable, the structure is suitable for the demands of various initial positions.

Description

Technical field [0001] The invention relates to a measuring device used for wind tunnel experiments, in particular to a free vibration suspension structure of a bridge segment model. Background technique [0002] The aerodynamic derivative is an important parameter to describe the aerodynamic performance of the bridge section, and it plays a vital role in the expression of aerodynamic self-excited force and flutter analysis. At present, the research on the mechanism of bridge flutter is often based on flutter analysis, especially the two-dimensional flutter analysis based on the measured aerodynamic derivative is an important means to reveal the macroscopic mechanism of bridge flutter. For a long time, aerodynamic derivative identification and flutter analysis have attracted the attention of the wind engineering community due to the dual difficulties in experiment and theory, and they are also a hotspot in the research of bridge wind engineering. The actual aerodynamic derivative...

Claims

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Application Information

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IPC IPC(8): G01M9/04
Inventor 辛大波李惠刘玉斌郭安薪高永生孙瑛陈文礼武岳
Owner HARBIN INST OF TECH
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